Theoretical and experimental (wind tunnel) studies of engine nozzle characteristics as well as of engine/airframe aerodynamic interaction are summarized. Results significant to fighter aircraft configuration optimization are identified. Wind tunnel experiment design is also critically assessed. Results emphasized concern: experimental data for parameters influencing afterbody drag; theoretical and construction concepts of variable 'CONDI' nozzles; theoretical methods for the correction of wind tunnel data; the synthesis of inlet drag; and investigations of jet decay structures.
Final Report on the Fuefo-4 Major Theme: Interference Drag with Airframe/Engine Integration on Fighter Aircraft Abschlussbereicht Zum Ruefo-4 Rahmenthema 'Interferenzwiderstand bei der Zellen-/Treibwerksintegration von Kampfflugzeugen'
1979
182 pages
Report
Keine Angabe
Englisch
Airframe-Propulsion Integration for Fighter Aircraft
AIAA | 1983
|Interfrerenzwiderstand bei der Zellen-/Triebwerksintegration von Kampfflugzeugen
Tema Archiv | 1979
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